For purposes of parameter identification, a class of N-degree of freedom dynamical systems are decoupled, to a single degree of freedom subsystem. This is achieved by utilizing all measured accelerations, and a coordinate transformation. In cases where additional data of strains or displacements are available, the decoupled equations are further simplified. The merits of this decoupling are clearly indicated.


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    Titel :

    Identification of Structural Component Failures Under Dynamic Loading


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Hart, Gary C. (Autor:in) / Simonian, Stepan (Autor:in)

    Kongress:

    Aerospace Meeting ; 1977



    Erscheinungsdatum :

    01.02.1977




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





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